View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 68231U 26145.62201863 +.00000000 +00000-0 +66645-3 0 00009
2 68231 97.2883 21.1507 0002788 95.3709 264.7852 15.33474043 01
| Epoch (UTC): | 25 May 2026 14:55:42 |
| Eccentricity: | 0.0002788 |
| inclination: | 97.2883° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 21.1507° |
| argument of perigee: | 95.3709° |
| revolutions per day: | 15.33474043 |
| mean anomaly at epoch: | 264.7852° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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